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Trubshaw, B., Concorde: the Inside Story, Sutton Publishing Limited, Phoenix Mill, Thrupp, Stroud, Gloucestershire, 2000.
Chudoba, B., Coleman, G., Oza, A. and Czysz, P. A., What Price Supersonic Speed? A Design Anatomy of Supersonic Transportation Part1, The Aeronautical Journal, 2008, 112(1129), 141-151.
Chudoba, B., Oza, A., Coleman, G. and Czysz, P. A., What Price Supersonic Speed? An Applied Market Research Case Study Part2, The Aeronautical Journal, 2008, 112(1130), 219-231.
Robert, J. M., A Supersonic Business-Jet Concept Designed for Low Sonic Boom, NASA TM-2003-212435, 2003.
Yoshida, K. and Makino, Y., Aerodynamic Design of Unmanned and Scaled Supersonic Experimental Airplane in Japan, Proceedings of the ECCOMAS 2004, Finland, 2004.
Makino, Y. and Kroo, I., Robust Objective Functions for Sonic-Boom Minimization, Journal of Aircraft, 2006, 43(5), 1301-1306.
Makino, Y., Aoyama, T., Iwamiya, T., Watanuki, T. and Kubota, H., Numerical Optimization of Fuselage Geometry to Modify Sonic-Boom Signature, Journal of Aircraft, 1999, 36(4), 668-674.
FAR 91.817, Part 91, General Operating and Flight Rules Subpart I - Operating Noise Limits, Federal Airworthiness Administration, Department of Transportation.
Pawlowski, J. W., Graham, D. H., Boccadoro, C, H., Coen, P. G. and Maglieri, D. J., Origins and Overview of the Shaped Sonic Boom Demonstration Program, AIAA Paper, AIAA-2005-0005, 2005.
Plotkin, K. J., Haering, E. A. Jr., Murray, J. E., Maglieri, D. J., Salamone, J., Sullivan, B. M. and Schein, D., Ground Data Collection of Shaped Sonic Boom Experiment Aircraft Pressure Signatures, AIAA Paper, AIAA-2005-0010, 2005.
Plotkin, K. J., Martin, R., Maglieri, D. J., Haering, E. A. Jr. and Murray, J. E., Pushover Focus Booms from the Shaped Sonic Boom Demonstrator, AIAA Paper, AIAA-2005-0011, 2005.
Morgenstern, J. M., Arslan, A., Lyman V. and Vadyak, J., F-5 Shaped Sonic Boom Demonstrator's Persistence of Boom Shaping Reduction through Turbulence, AIAA Paper, AIAA-2005-0012, 2005.
Henne, P. A., Case for Small Supersonic Civil Aircraft, Journal of Aircraft, 2005, 42(3), 765-774.
Howe, D. C., Improved Sonic Boom Minimization with Extendable Nose Spike, AIAA Paper, AIAA-2005-1014, 2005.
Cowart, R. and Grindle, T., An Overview of the Gulfstream / NASA Quiet Spike™ Flight Test Program, AIAA Paper, AIAA-2008-0123, 2008.
Howe, D. C., Simmons, III, F. and Freund, D., Development of the Gulfstream Quiet Spike™ for Sonic Boom Minimization, AIAA Paper, AIAA-2008-0124, 2008.
Howe, D. C., Waithe, K. A. and Haering, E. A. Jr., Quiet Spike™ Near Field Flight Test Pressure Measurements with Computational Fluid Dynamics Comparisons, AIAA Paper, AIAA-2008-0128, 2008.
Smith, H., A Review of Supersonic Business Jet Design Issues, The Aeronautical Journal, 2007, 111(1126), 761-776.
Kusunose, K., A New Concept in the Development of Boomless Supersonic Transport, Proceedings of the First International Conference on Flow Dynamics, Sendai, Japan, 2004, 46-47.
Kusunose, K., Matsushima, K., Goto, Y., Yamashita, H., Yonezawa, M., Maruyama, D. and Nakano, T., A Fundamental Study for the Development of Boomless Supersonic Transport Aircraft, AIAA Paper, AIAA-2006-0654, 2006.
Liepmann, H. W. and Roshko, A., Elements of Gas Dynamics, John Wiley & Sons, Inc., New York, 1957, 107-123, 389.
Matsushima, K., Kusunose, K., Maruyama, D. and Matsuzawa, T., Numerical Design and Assessment of a Biplane as Future Supersonic Transport - Revisiting Busemann's Biplane, Proceedings of the 25th ICAS Congress, ICAS 2006-3.7.1, 1-10, Hamburg, Germany, 2006.
Maruyama, D., Matsushima, K., Kusunose, K. and Nakahashi, K., Aerodynamic Design of Biplane Airfoils for Low Wave Drag Supersonic Flight, AIAA Paper, AIAA-2006-3323, 2006.
Maruyama, D., Matsushima, K., Kusunose, K. and Nakahashi, K., Aerodynamic Design of Threedimensional Low Wave-drag Biplanes Using Inverse Problem Method, AIAA Paper, AIAA-2008-0289, 2008.
Kusunose, K., Matsushima, K., Obayashi, S., Furukawa, T., Kuratani, N., Goto, Y., Maruyama, D., Yamashita, H. and Yonezawa, M., Aerodynamic Design of Supersonic Biplane: Cutting Edge and Related Topics, The 21st Century COE Program, International COE of Flow Dynamics Lecture Series, Vol. 5, Tohoku University Press, Sendai, Japan, 2007.
Yonezawa, M., Yamashita, H., Obayashi, S. and Kusunose, K., Investigation of Supersonic Wing Shape Using Busemann Biplane Airfoil, AIAA Paper, AIAA-2007-0686, 2007.
Kuratani, N., Ogawa, T., Yamashita, H., Yonezawa, M. and Obayashi, S., Experimental and Computational Fluid Dynamics around Supersonic Biplane for Sonic-Boom Reduction, AIAA Paper, AIAA-2007-3674, 2007.
Yamashita, H., Yonezawa, M., Obayashi, S. and Kusunose, K., A Study of Busemann-type Biplane for Avoiding Choked Flow, AIAA Paper, AIAA-2007-0688, 2007.
Aksel, M. H. and Eralp, O. C., Gas Dynamics, Prentice Hall Inc., Englewood Cliffs, 1994, Chap. 5, 186-195.
Van Wie, D. M., Kwok, F. T. and Walsh, R. F., Starting Characteristics of Supersonic Inlets, AIAA Paper, AIAA-1996-2914, 1996.
Takaki, R., Yamamoto, K., Yamane, T., Enomoto, S. and Mukai, J., The Development of the UPACS CFD Environment, Proceedings of the 5th International Symposium, ISHPC 2003, Springer, Tokyo, 2003, 307-319.
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International Journal of Emerging Multidisciplinary Fluid Sciences

International Journal of Emerging Multidisciplinary Fluid Sciences

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